An optimal design methodology for a class of air-breathing launch vehicles
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1980. === MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO. === Vita. === Includes bibliographical references. === by Philip David Hattis. === Ph.D.
Main Author: | Hattis, Philip David |
---|---|
Other Authors: | Wallace E. Vander Velde...et al. |
Format: | Others |
Language: | English |
Published: |
Massachusetts Institute of Technology
2005
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/15816 |
Similar Items
-
A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization
by: Steffens, Michael J.
Published: (2014) -
Time-domain finite elements in optimal control with application to launch-vehicle guidance
by: Bless, Robert R.
Published: (2008) -
Optimal trajectory reconfiguration and retargeting for the X-33 reusable launch vehicle
by: Shaffer, Patrick J.
Published: (2012) -
Launch Vehicle Trajectory Optimization In Parallel Processors
by: Anand, J K
Published: (2012) -
Dynamics And Stability Of A Launch Vehicle
by: Trikha, Manish
Published: (2011)